IP Library Granted Patent US 7,866,575
Granted Patent B2
US 7,866,575 · App. 12/351,931 · Granted Jan 11, 2011

Pressure actuated fuel injector

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Quick Facts
Patent No.
US 7,866,575
App. No.
12/351,931
Granted
Jan 11, 2011
Kind
B2
Abstract

An engine assembly may include a fuel injector having a housing, an actuation mechanism, and a valve member. The housing may define a high pressure region, a low pressure region, a longitudinal bore, and a valve seat having an aperture extending therethrough. The actuation member may be disposed within the longitudinal bore and may include a first axial end surface. The valve mechanism may include a second axial end surface abutting the first axial end surface. The first and second axial end surfaces define an outer contact perimeter and a chamber within the outer contact perimeter. A radial surface area defined by the chamber formed by the first and second axial end surfaces may be at least 25 percent of a radial surface area defined within the outer contact perimeter.

Claims (28)

1. A fuel injector comprising:

a housing defining a high pressure region, a low pressure region, a longitudinal bore, and a valve seat including a valve seat surface and an aperture, the valve seat surface being in fluid communication with the low pressure region and the aperture extending through the valve seat surface and being in communication with the high pressure region;

an actuation member disposed within the longitudinal bore for axial displacement therein and including a first axial end surface; and

a valve mechanism axially displaceable between first and second positions, the valve mechanism abutting the valve seat in the first position to seal the aperture from communication with the low pressure region, the valve mechanism being displaced from the valve seat in the second position to provide communication between the low and high pressure regions through the aperture, the valve mechanism including a second axial end surface abutting the first axial end surface of the actuation member, the first and second axial end surfaces defining an outer contact perimeter and a chamber within the outer contact perimeter, a radial surface area of the chamber formed by the first and second axial end surfaces being at least 25 percent of a radial surface area defined within the outer contact perimeter.

2. The fuel injector of claim 1 , wherein the first axial end surface is generally planar within the outer contact perimeter and the second axial end surface includes a recess within the outer contact perimeter to form the chamber.

3. The fuel injector of claim 1 , wherein the first axial end surface includes a first recess within the outer contact perimeter to form the chamber.

4. The fuel injector of claim 3 , wherein the second axial end surface includes a second recess within the outer contact perimeter, the first and second recesses forming the chamber.

5. The fuel injector of claim 3 , wherein the second axial end surface is generally planar within the outer contact perimeter.

6. The fuel injector of claim 1 , wherein the radial surface area of the chamber formed by the first and second axial end surfaces is between 50 and 95 percent of the radial surface area defined by the outer contact perimeter.

7. The fuel injector of claim 1 , wherein the first and second axial end surfaces are radially displaceable relative to one another.

8. The fuel injector of claim 1 , wherein the valve mechanism includes a valve holder and a valve member, the valve holder including the second axial end surface at a first axial end and a third axial end surface at a second axial end opposite the first axial end, the third axial end surface including a recess housing the valve member.

9. The fuel injector of claim 8 , wherein the valve member includes a ball.

10. The fuel injector of claim 1 , further comprising an injection valve, the housing including an injection nozzle opening, the injection valve being displaceable from a third position where the injection valve seals the injection nozzle opening to a fourth position where the injection valve opens the nozzle opening, the injection valve being displaced from the third position to the fourth position by fuel pressure when the valve mechanism is displaced from the first position to the second position.

11. An engine assembly comprising:

an engine structure defining a cylinder bore; and

a fuel injector supported by the engine structure and in communication with the cylinder bore, the fuel injector including:

a housing defining a high pressure region, a low pressure region, a longitudinal bore, and a valve seat including a valve seat surface and an aperture, the valve seat surface being in fluid communication with the low pressure region and the aperture extending through the valve seat surface and being in communication with the high pressure region;

an actuation member disposed within the longitudinal bore for axial displacement therein and including a first axial end surface; and

a valve mechanism axially displaceable between first and second positions, the valve mechanism abutting the valve seat in the first position to seal the aperture from communication with the low pressure region, the valve mechanism being displaced from the valve seat in the second position to provide communication between the low and high pressure regions through the aperture, the valve mechanism including a second axial end surface abutting the first axial end surface of the actuation member, the first and second axial end surfaces defining an outer contact perimeter and a chamber within the outer contact perimeter, a radial surface area of the chamber formed by the first and second axial end surfaces being at least 25 percent of a radial surface area defined within the outer contact perimeter.

12. The engine assembly of claim 11 , wherein the first axial end surface is generally planar within the outer contact perimeter and the second axial end surface includes a recess within the outer contact perimeter to form the chamber.

13. The engine assembly of claim 11 , wherein the first axial end surface includes a first recess within the outer contact perimeter to form the chamber.

14. The engine assembly of claim 13 , wherein the second axial end surface includes a second recess within the outer contact perimeter, the first and second recesses forming the chamber.

15. The engine assembly of claim 13 , wherein the second axial end surface is generally planar within the outer contact perimeter.

16. The engine assembly of claim 11 , wherein the radial surface area of the chamber formed by the first and second axial end surfaces is between 50 and 95 percent of the radial surface area defined by the outer contact perimeter.

17. The engine assembly of claim 11 , wherein the first and second axial end surfaces are radially displaceable relative to one another.

18. The engine assembly of claim 11 , wherein the valve mechanism includes a valve holder and a valve member, the valve holder including the second axial end surface at a first axial end and a third axial end surface at a second axial end opposite the first axial end, the third axial end surface including a recess housing the valve member.

19. The engine assembly of claim 18 , wherein the valve member includes a ball.

20. The engine assembly of claim 11 , further comprising an injection valve, the housing including an injection nozzle opening, the injection valve being displaceable from a third position where the injection valve seals the injection nozzle opening to a fourth position where the injection valve opens the nozzle opening, the injection valve being displaced from the third position to the fourth position by fuel pressure when the valve mechanism is displaced from the first position to the second position.

Assignments (8)
RELEASE OF SECURITY INTEREST Recorded Nov 7, 2014
From: WILMINGTON TRUST COMPANY
To: GM GLOBAL TECHNOLOGY OPERATIONS LLC
Reel/Frame 034185/0789 →
CHANGE OF NAME Recorded Feb 10, 2011
From: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
To: GM GLOBAL TECHNOLOGY OPERATIONS LLC
Reel/Frame 025781/0245 →
SECURITY AGREEMENT Recorded Nov 8, 2010
From: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
To: WILMINGTON TRUST COMPANY
Reel/Frame 025324/0515 →
RELEASE OF SECURITY INTEREST Recorded Nov 5, 2010
From: UAW RETIREE MEDICAL BENEFITS TRUST
To: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
Reel/Frame 025315/0046 →
RELEASE OF SECURITY INTEREST Recorded Nov 4, 2010
From: UNITED STATES DEPARTMENT OF THE TREASURY
To: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
Reel/Frame 025246/0056 →
SECURITY AGREEMENT Recorded Aug 28, 2009
From: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
To: UAW RETIREE MEDICAL BENEFITS TRUST
Reel/Frame 023162/0237 →
SECURITY AGREEMENT Recorded Aug 27, 2009
From: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
To: UNITED STATES DEPARTMENT OF THE TREASURY
Reel/Frame 023156/0313 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jan 12, 2009
From: STRAUB, ROBERT D.
To: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
Reel/Frame 022088/0356 →